Tables of Airspeed, Altitude, and Mach Number Based on Latest International Values for Atmospheric Properties and Physical ConstantsNational Aeronautics and Space Administration, 1961 - 37 pages Pressure-airspeed tables based on the latest established value for the nautical mile and the physical constants and atmospheric properties adopted for the International Civil Aviation Organization (ICAO) standard atmosphere are presented. Impact pressures are given for airspeeds up to 1,000 knots and 1,100 miles per hour. Pre sure-altitude tables are given for altitudes up to 100,000 geopotential feet. Mach number in terms of the ratio impact pressure to freestream static pressure for Mach numbers from 0.10 to 5.00 are given. True airspeeds are tabulated for calibrated airspeeds from 100 to 1,000 knots and for altitudes from 0 to 100,000 geopotential feet. |
Common terms and phrases
100,000 geopotential feet 9 mph acceleration of gravity airspeed indicators airspeed tables altimeters ALTITUDE H altitude tables ambient air CALIBRATED AIRSPEED VC computation Concluded Calibrated airspeed constants and atmospheric Continued These values FOOT FOR VALUES FREE-AIR TEMPERATURE geopo given in table H IN GEOPOTENTIAL height hour and knots ICAO standard atmosphere IMPACT PRESSURE 9c INCHES OF MERCURY Langley Field latest accepted values MACH NUMBER Continued MACH NUMBER TABLES mercury and pounds MERCURY FOR VALUES meters miles per hour molecular weight NACA Rep nautical mile physical constants pitot tube POUNDS PER SQUARE PRESSURE ALTITUDE PRESSURE TO STATIC pressure-airspeed tables pressure-altitude tables qc/P FOR VALUES RATIO OF IMPACT recovery factor references 9 speed of sound SQUARE FOOT standard sea-level conditions STATIC PRESSURE qc/P TABLE VII Tables and Data tables of references true airspeed VALUES OF CALIBRATED VALUES OF MACH VALUES OF PRESSURE VC IN KNOTS VC IN MILES Яс